Honeycomb Parameter-Sensitive Predictive Models for Ballistic Limit of Spacecraft Sandwich Panels Subjected to Hypervelocity Impact at Normal Incidence-Reference-Cited by-同舟云学术

Honeycomb Parameter-Sensitive Predictive Models for Ballistic Limit of Spacecraft Sandwich Panels Subjected to Hypervelocity Impact at Normal Incidence

Published:2022-07 Issue:4 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Carriere Riley¹^ORCID,Cherniaev Aleksandr²^ORCID

Affiliation:

1. Research Assistant, Dept. of Mechanical, Automotive, and Materials Engineering, Univ. of Windsor, Windsor, ON, Canada N9B 3P4. ORCID:

2. Assistant Professor, Dept. of Mechanical, Automotive, and Materials Engineering, Univ. of Windsor, Windsor, ON, Canada N9B 3P4 (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001436

Reference38 articles.

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3. Projectile Shape Effects in Hypervelocity Impact of Honeycomb-Core Sandwich Structures

4. ASM International. 2002. Atlas of stress-strain curves. 2nd ed. Materials Park, OH: American Society for Metals International.

5. A Modular Design Concept For Small Satellites

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